IRIDIUM 106, 41917
Orbit data source: Space-Track
IRIDIUM 106, 41917 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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41917 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 106
1 41917U 17003A 25345.06933236 -.00000115 00000-0 -48054-4 0 9998
2 41917 86.3990 167.1514 0002134 100.3173 259.8264 14.34216989466244Epoch: 2025-12-11T01:39Z
TLE epoch observation values (Epoch: 2025-12-11T01:39:50.315Z)
Latitude
0.00001°
Longitude
62.16115°
Altitude
780.991 km
Speed
7.463 km/s
True Right ascension
11h 08m 36s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
08:47:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.161 km
Perigee altitude
773.108 km
Semi-major axis
7,152.771 km
Eccentricity
0.00021
Inclination
86.399°
RAAN
167.1514°
Arg. of periapsis
100.3173°
True anomaly
259.80233°
Mean anomaly
259.8264°
Eccentric anomaly
259.81437°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000048054
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 106 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-11 11:50:37.818Z | 125.658° SE | 2025-12-11 11:53:37.818Z | 87.106° E | 20.162° | 2025-12-11 11:57:37.818Z | 34.38° NE |
| 8 mins | 2025-12-11 13:30:37.818Z | 213.663° SW | 2025-12-11 13:34:37.818Z | 284.557° WNW | 32.742° | 2025-12-11 13:38:37.818Z | 344.234° N |
| 8 mins | 2025-12-12 00:01:37.818Z | 17.344° NNE | 2025-12-12 00:04:37.818Z | 75.965° E | 37.157° | 2025-12-12 00:09:37.818Z | 158.562° S |
| 4 mins | 2025-12-12 01:43:37.818Z | 300.877° NW | 2025-12-12 01:44:37.818Z | 287.12° WNW | 16.8° | 2025-12-12 01:47:37.818Z | 247.339° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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